IMAGING ASSISTED GAS TURBINE ANTI-ICING SYSTEM
First Claim
Patent Images
1. A method comprising:
- receiving image data from a camera coupled to an air intake system of a gas turbine engine, wherein the image data corresponds to an air passage of the air intake system;
comparing the received image data to reference image data of the air intake system; and
generating an icing notification based at least in part on the comparison when a difference between the received image data and reference image data is greater than an icing threshold.
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Abstract
A method includes receiving image data from a camera coupled to an air intake system of a gas turbine engine. The image data corresponds to an air passage of the air intake system. The method also includes comparing the received image data to reference image data of the air intake system. The method also includes generating an icing notification based at least in part on the comparison when a difference between the received image data and reference image data is greater than an icing threshold.
15 Citations
20 Claims
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1. A method comprising:
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receiving image data from a camera coupled to an air intake system of a gas turbine engine, wherein the image data corresponds to an air passage of the air intake system; comparing the received image data to reference image data of the air intake system; and generating an icing notification based at least in part on the comparison when a difference between the received image data and reference image data is greater than an icing threshold. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. A system comprising:
a controller, comprising; one or more tangible, non-transitory, machine-readable media collectively storing one or more sets of instructions; and one or more processing devices configured to execute the one or more sets of instructions to; receive image data from a camera coupled to an air intake system of a gas turbine engine, wherein the image data corresponds to an air passage of the air intake system; compare the received image data to reference image data of the air intake system; and generate an icing notification based at least in part on the comparison when a difference between the received image data and reference image data is greater than an icing threshold. - View Dependent Claims (12, 13, 14, 15, 16)
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17. A system comprising:
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a gas turbine engine comprising an air intake system, the air intake system comprising an air passage; a camera coupled to the air intake system and configured to image the air passage of the air intake system; and a controller communicatively coupled to the camera and configured to; receive image data from the camera, wherein the image data corresponds to the air passage; compare the received image data to reference image data of the air intake system; and generate an icing notification based at least in part on the comparison when a difference between the received image data and reference image data is greater than an icing threshold. - View Dependent Claims (18, 19, 20)
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Specification